View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 85U 61004C 23336.39979382 .00097206 00000-0 14661-1 0 9994
2 85 38.7509 349.5517 0289827 7.0249 353.4444 14.48793077111571
| Epoch (UTC): | 02 December 2023 09:35:42 |
| Eccentricity: | 0.0289827 |
| inclination: | 38.7509° |
| perigee height: | 523 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 349.5517° |
| argument of perigee: | 7.0249° |
| revolutions per day: | 14.48793077 |
| mean anomaly at epoch: | 353.4444° |
| orbit number at epoch: | 11157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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